Structural Engineering and Mechanics

  • 제73권2호
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  • Pages.181-190
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  • 2020
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  • 1225-4568(pISSN)
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  • 1598-6217(eISSN)
테크노프레스 (Techno-Press)
권호 표지
DOI QR코드

DOI QR Code

Non-Linear dynamic pulse buckling of laminated composite curved panels

  • Keshav, Vasanth (Department of Civil Engineering, BITS Pilani, Pilani Campus) ;
  • Patel, Shuvendu N. (Department of Civil Engineering, BITS Pilani, Pilani Campus)
  • 투고 : 2018.07.24
  • 심사 : 2019.10.05
  • 발행 : 2020.01.25
⟨ 이전 논문 다음 논문 ⟩

초록

In this paper, non-linear dynamic buckling behaviour of laminated composite curved panels subjected to dynamic in-plane axial compressive loads is studied using finite element methods. The work is carried out using the finite element software ABAQUS. The curved panels are modelled with S4R element and the nonlinear dynamic equilibrium equations are solved using the ABAQUS/Explicit algorithm. The effect of aspect ratio, radius of curvature and thickness are studied. The importance of orientation of plies in the direction of loading is also reiterated in this study. Vol'mir's criterion is used to calculate the dynamic buckling loads. The panels are subjected to rectangular pulse load of various amplitude and durations and the responses are observed. For particular loading amplitude, a critical value of loading duration is observed beyond which the variation of dynamic buckling load is insignificant. It is also observed that, the value of dynamic bucking load reduces as the loading duration is increased though the reduction is not much after a particular loading duration.

키워드

과제정보

연구 과제 주관 기관 : Council of Scientific and Industrial Research (CSIR)

참고문헌

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